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Aerodynamic Design Study for Multi-Lifting Surfaces

Yang, Qingzhen and Streit, Thomas and Wichmann, Georg (2005) Aerodynamic Design Study for Multi-Lifting Surfaces. In: Conference Proccedings, CEAS/KATnet Conference on Key Aerodynamic Technologies June 2005, pp. 1-8. CEAS/KATnet Conference on Key Aerodynamic Technologies, 20 - 22 June 2005, Bremen, Germany, 2005-06-20-2005-06-22, Bremen.

Full text not available from this repository.

Abstract

An aerodynamic design method and corresponding codes have been developed for three dimensional multi-lifting surfaces at transonic flow. It is based on the "iterative residual coreection" concept that is succesfully used for transonic wing and subsonic multi-lifting surface design. An upwind scheme is introduced into the governing equations for the multi-lifting surface design method and schwitched on automatically when supersonic flow appears on the surface. A series of interface codes have been programmed, including a target pressure modification tool. The transonic multi-lifting aerodynamic design software includes the improved inverse aerodynamic design code, the DLR-TAU code for Navier-Stokes/Euler CFD analyis and interface codes. Two cases of a canard-wing configuration have been tested to validate the methods and codes. The results show that the analysis/design iterations converge at higher transonic flow.

Document Type:Conference or Workshop Item (Speech, Paper)
Title:Aerodynamic Design Study for Multi-Lifting Surfaces
Authors:
AuthorsInstitution or Email of Authors
Yang, QingzhenNorthwestern Polytechnical University, Xi'an, China
Streit, ThomasUNSPECIFIED
Wichmann, GeorgUNSPECIFIED
Date:June 2005
Journal or Publication Title:Conference Proccedings, CEAS/KATnet Conference on Key Aerodynamic Technologies June 2005
Refereed publication:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-8
Status:Published
Keywords:inverse design method, multi-lifting surface design, iterative residual coreection, DLR-TAU solver, Navier-Stokes/Euler numerical solution
Event Title:CEAS/KATnet Conference on Key Aerodynamic Technologies, 20 - 22 June 2005, Bremen, Germany
Event Location:Bremen
Event Type:international Conference
Event Dates:2005-06-20-2005-06-22
Organizer:Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V. (DGLR)
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:Aircraft Research
DLR - Research area:Aeronautics
DLR - Program:L AR - Aircraft Research
DLR - Research theme (Project):L - Flight Physics
Location: Braunschweig
Institutes and Institutions:Institute of Aerodynamics and Flow Technology > Configuration Design
Deposited By: Dr.rer.nat. Thomas Streit
Deposited On:11 Jan 2007
Last Modified:27 Apr 2009 13:25

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